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The Model 53 was an airliner version of the Model 52 Condor B-2 bomber, also introduced in 1929. It was a large, equal span, three bay biplane with parallel pairs of interplane struts. Its wings had a rectangular plan out to rounded tips. Like the rest of the aircraft, they had an all-metal structure and were fabric covered.
Data from Jane's all the World's Aircraft 2000/01 General characteristics Capacity: 2 Length: 6.08 m (19 ft 11 in) Wingspan: 10.60 m (34 ft 9 in) Height: 2.30 m (7 ft 7 in) Wing area: 14.84 m 2 (159.7 sq ft) Empty weight: 265 kg (584 lb) minimum Max takeoff weight: 450 kg (992 lb) Ultralight category limit Fuel capacity: 50L (11.0 Imp gal, 13.2 US gal) Powerplant: 1 × Rotax 582 UL-DCDI two ...
Avia Solutions Group is a holding company with subsidiaries specializing in various aircraft related businesses, including aircraft maintenance; repair and overhaul (MRO); leasing and trading of aircraft; ground handling and fueling; aviation training; personnel resourcing; and business and corporate aviation, in addition to its primary function as an ACMI provider. [24]
[citation needed] The designation "Condor" was chosen because, like the condor bird, the Fw 200 had a very long wingspan compared to other planes of its era, to facilitate high-altitude flight. During June 1936, following discussions between Tank, Stüssel and Carl August von Gablenz, Deutsche Luft Hansa issued a specification.
In 2021, the company reported profits of €43.6m after tax and revenue of €1,131.5m with cash reserves increasing to 46.3% year on year to €192.2m. [3] ASL acquired 100% ownership of ASL Maintenance (formally X-air services) on 9 August 2022. [12] The company was previously jointly-owned on a fifty-fifty basis by ASL and Sabena technics.
The aircraft was designed to comply with the US FAR 103 Ultralight Vehicles rules, including the category's maximum empty weight of 254 lb (115 kg). The aircraft has a standard empty weight of 240 lb (109 kg). It features a cable-braced high-wing, open cockpit, tricycle landing gear and a single engine in pusher configuration.
In 1932 the Air Ministry initiated a conversion of the Condor petrol engine to the compression ignition system. The conversion was developed at the Royal Aircraft Establishment, Farnborough, with the co-operation of Rolls-Royce Ltd. Engine layout, bore, and stroke remained the same as for the petrol version; the compression ratio increased to 12.5:1.
The fuselage was lengthened by 8 in (203 mm), chiefly by moving the cockpit further forward, at the cost of a 7 lb (3.2 kg) increase in weight. The trailing edge of the rudder was curved outwards and a very small dorsal fillet added. Minor undercarriage changes were also made. Named Condor 2, the rebuilt aircraft first flew on 13 August 1960. [1]